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Turbopump Mechanical Engineer [High-Thrust Rocket Engine](m/w/x)
Thermomechanical design of cryogenic pump assemblies for high-thrust propulsion systems, supervising subcontractors. Master's in Mechanical/Aerospace Engineering and rotordynamics understanding required. Relocation assistance and visa sponsorship available.
Requirements
- Master's degree in Mechanical Engineering, Aerospace Engineering, related technical discipline, or bachelor's degree with substantial relevant experience
- Strong fundamentals in thermodynamics and mechanical design
- Understanding of machine dynamics problems like rotordynamics
- Good knowledge of materials
- Good understanding of manufacturing methods and constraints
- Proficiency in 3D CAD software and drafting
- Experience writing software/scripts (e.g., Python)
- Strong collaboration skills
- Strong oral and written communication skills
- Strong analysis and problem-solving skills
- Strong research and information inference skills
- Drive for excellence and time management
- Proficiency in organization and task prioritization
- Fluency in English
- Strong understanding of liquid-propellant rocket engines
- Proven experience with fast-rotating machinery
- Hands-on hardware development experience
Tasks
- Make and document consequential turbomachinery design decisions
- Proactively assist development engineers with design conception, refinement, and validation
- Design cryogenic pump components and assemblies thermomechanically
- Apply specifications and best practices to designs
- Supervise external subcontractors
- Communicate with suppliers
- Perform analytical modeling of geometric and mechanical problems
- Implement solutions in programs
Work Experience
- approx. 1 - 4 years
Education
- Bachelor's degreeOR
- Master's degree
Languages
- English – Business Fluent
Tools & Technologies
- 3D CAD software
- Python
Benefits
Other Benefits
- Relocation assistance
- Visa sponsorship
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Turbopump Mechanical Engineer [High-Thrust Rocket Engine](m/w/x)
Thermomechanical design of cryogenic pump assemblies for high-thrust propulsion systems, supervising subcontractors. Master's in Mechanical/Aerospace Engineering and rotordynamics understanding required. Relocation assistance and visa sponsorship available.
Requirements
- Master's degree in Mechanical Engineering, Aerospace Engineering, related technical discipline, or bachelor's degree with substantial relevant experience
- Strong fundamentals in thermodynamics and mechanical design
- Understanding of machine dynamics problems like rotordynamics
- Good knowledge of materials
- Good understanding of manufacturing methods and constraints
- Proficiency in 3D CAD software and drafting
- Experience writing software/scripts (e.g., Python)
- Strong collaboration skills
- Strong oral and written communication skills
- Strong analysis and problem-solving skills
- Strong research and information inference skills
- Drive for excellence and time management
- Proficiency in organization and task prioritization
- Fluency in English
- Strong understanding of liquid-propellant rocket engines
- Proven experience with fast-rotating machinery
- Hands-on hardware development experience
Tasks
- Make and document consequential turbomachinery design decisions
- Proactively assist development engineers with design conception, refinement, and validation
- Design cryogenic pump components and assemblies thermomechanically
- Apply specifications and best practices to designs
- Supervise external subcontractors
- Communicate with suppliers
- Perform analytical modeling of geometric and mechanical problems
- Implement solutions in programs
Work Experience
- approx. 1 - 4 years
Education
- Bachelor's degreeOR
- Master's degree
Languages
- English – Business Fluent
Tools & Technologies
- 3D CAD software
- Python
Benefits
Other Benefits
- Relocation assistance
- Visa sponsorship
Like this job?
BetaYour Career Agent finds similar jobs for you every day.
About the Company
The Exploration Company
Industry
Aerospace
Description
The company is developing, producing, and operating Nyx, a modular and reusable space orbital vehicle.
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